STARLINK-35044, 65536
Orbit data source: Space-Track
STARLINK-35044, 65536 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sat, 06 Sep 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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65536 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-35044
1 65536U 25200S 26171.45481036 -.00000996 00000-0 -65070-4 0 9990
2 65536 97.3357 239.9949 0002510 117.9940 242.1541 15.05656442 44594Epoch: 2026-06-20T10:54Z
TLE epoch observation values (Epoch: 2026-06-20T10:54:55.615Z)
Latitude
-0.00007°
Longitude
167.59399°
Altitude
553.377 km
Speed
7.585 km/s
True Right ascension
15h 59m 58s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:14:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.211 km
Perigee altitude
544.735 km
Semi-major axis
6,924.61 km
Eccentricity
0.00025
Inclination
97.3357°
RAAN
239.9949°
Arg. of periapsis
117.994°
True anomaly
242.12867°
Mean anomaly
242.1541°
Eccentric anomaly
242.14139°
Mean motion
3.76661 °/min
Orbital period
95.58 mins
BSTAR
-0.00006507
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Other satellites on launch #200 in the year 2025 (2025-09-06 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.STARLINK-35044 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 04:34:42.001Z | 164.574° S | 2026-06-21 04:38:42.001Z | 7.385° NNE | 43.586° | 2026-06-21 04:41:42.001Z | 349.954° N |
| 6 mins | 2026-06-21 17:47:42.001Z | 352.949° N | 2026-06-21 17:49:42.001Z | 306.351° NW | 36.549° | 2026-06-21 17:53:42.001Z | 210.937° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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